An innovative route from wind tunnel experiments to flight dynamics analysis for a highly swept flying wing

Author:

Schwithal J.ORCID,Rohlf D.,Looye G.,Liersch C. M.

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference30 articles.

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2. Liersch, C. M., Huber, K.: Conceptual design and aerodynamic analyses of a generic UCAV configuration, 32nd AIAA applied aerodynamics conference, AIAA-2014-2001, Atlanta, GA, USA (2014)

3. Rohlf, D., Schmidt, S., Irving, J.: Stability and control analysis for an unmanned aircraft configuration using system-identification techniques. J. Aircr. 49(6), 1597–1609 (2012)

4. Nathman, J. K.: VSAERO—a computer program for calculating the nonlinear aerodynamic characteristics of arbitrary configurations, users’ manual version 7.2, Redmond, WA, USA (2007)

5. Nagel, B., Böhnke, D. Gollnick, V., Schmollgruber, P., Rizzi, A., La Rocca, G., Alonso, J.J.: Communication in aircraft design: can we establish a common language?, 28th international congress of the aeronautical sciences, Brisbane, Australia (2012)

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